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A flight investigation of the reduction of aileron operating force by means of fixed tabs and differential linkage, with notes on linkage design (1938)

NASA Technical Reports Server (NTRS) · leaf 24

An illustration from A flight investigation of the reduction of aileron operating force by means of fixed tabs and differential linkage, with notes on linkage design, 1938, leaf 24
Figure 15.- The variation of stick force with, the sum of the upward and downward deflections of the two ailerons.

NASA Technical Reports Server (NTRS)

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